CALLISTO: on the design and development of a reusable first stage demonstrator
Open Access
- 3 March 2026
- journal article
- research article
- Published by Springer Nature in CEAS Space Journal
- p. 1-14
Abstract
CALLISTO is a collaborative project between JAXA, CNES, and DLR, focused on developing and operating a scaled reusable vertical-takeoff vertical-landing rocket stage demonstrator. This initiative is a crucial step for advancing reusable launch vehicle (RLV) technology in Europe and Japan. Significant strides have been made during the recently completed phase C of the project, particularly in aerodynamic modeling, guidance, navigation, and control design, landing dynamics, and flight domain definitions. These advancements facilitate the development of future operational vehicles and provide insights applicable to other RLV projects. This paper provides an update on the design and development status of the CALLISTO vehicle. It outlines the program objectives, focusing on mission design, vehicle life cycle, and their distinctions from legacy expendable launch vehicles in Europe and Japan. Details of the flight test plan, including in-flight experimentation, are elucidated, demonstrating incremental progress toward acquiring key technology and preparing for high-energy missions. Furthermore, the paper offers an overview of the CALLISTO vehicle’s development status, highlighting key architectural features such as load-carrying structures, avionics, rocket propulsion system, flight control systems, and approach and landing system. It underscores the milestones achieved over the past years and the progress toward the first flights. With a flight test campaign to be performed at Europe’s Spaceport in French Guiana, the CALLISTO project signifies a crucial step toward enhancing launch system affordability, competitiveness, versatility, and sustainability. This collaboration among three space organizations highlights the importance of shared expertise in advancing RLV technology and preparing for the next generation of launch vehicles.Keywords
Funding Information
- Bundesministerium für Wirtschaft und Klimaschutz
- Deutsches Zentrum für Luft- und Raumfahrt
- Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)
This publication has 11 references indexed in Scilit:
- The CALLISTO and ReFEx flight experiments at DLR - Challenges and opportunities of a wholistic approachActa Astronautica, 2024
- Aerothermal characterization of the CALLISTO vehicle during descentCEAS Space Journal, 2024
- Comparative analysis of European vertical landing reusable first stage conceptsCEAS Space Journal, 2024
- CALLISTO Reusable rocket stage demonstrator: consolidating the design2024
- Bayesian Models for Uncertainty Estimation in Aerodynamic Databases of Reusable Launch Vehicles2024
- Six-Degree-of-Freedom Rocket Landing Optimization via Augmented Convex–Concave DecompositionJournal of Guidance, Control, and Dynamics, 2024
- Unified-Loop Structured H-Infinity Control for Aerodynamic Steering of Reusable RocketsJournal of Guidance, Control, and Dynamics, 2023
- Applying Bayesian Inference to Estimate Uncertainties in the Aerodynamic Database of CALLISTO2023
- Advanced Modeling and Dynamic Stability Analysis of the Aerodynamic Control Surfaces of CALLISTO2023
- Onboard Guidance for Reusable Rockets: Aerodynamic Descent and Powered Landing2021